Roko Aero NG 4 ML, Operating Instructions Manual

Page: 51 / 69

6-6
Date of Issue: 04/2008 Revision: 1.0
WEIGHT & BALANCE REPORT
Forward C.G. Check
ITEM
WEIGHT
(kg)
ARM
(m)
MOMENT
(WEIGHTxARM)
A
IR
C
R
A
FT
E
MP
TY
CG
RIGHT MAIN
WHEEL
W
R
= 120,6 L
R
= 0,79 95274
LEFT MAIN
WHEEL
W
L
= 124,4 L
L
= 0,79 95274
NOSE WHEEL
W
N
= 103
L
N
= - 0,785
(negative arm)
- 80855
COMPUTED CG
EMPTY
Empty Weight:
W
E
= 348 kg
CG = 0,323m
25,5 % MAC
Aircraft moment:
112695